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Aircraft performance [2nd. ed.] (Record no. 567335)

MARC details
000 -LEADER
fixed length control field 01773 a2200217 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9781032245157
040 ## - CATALOGING SOURCE
Transcribing agency IIT Kanpur
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title eng
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.133
Item number Sa15a2
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name Sadraey, Mohammad H.
245 ## - TITLE STATEMENT
Title Aircraft performance [2nd. ed.]
Remainder of title an engineering approach
Statement of responsibility, etc Mohammad H. Sadraey
250 ## - EDITION STATEMENT
Edition statement 2nd ed.
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher CRC Press
Year of publication 2024
Place of publication Boca Raton
300 ## - PHYSICAL DESCRIPTION
Number of Pages xxv, 666p
500 ## - GENERAL NOTE
General note Instructor and Student Resources
520 ## - SUMMARY, ETC.
Summary, etc Aircraft Performance: An Engineering Approach, Second Edition introduces flight performance analysis techniques of fixed-wing air vehicles, particularly heavier-than-aircraft. It covers maximum speed, absolute ceiling, rate of climb, range, endurance, turn performance, and takeoff run.<br/><br/>Enabling the reader to analyze the performance and flight capabilities of an aircraft by utilizing only the aircraft weight data, geometry, and engine characteristics, this book covers the flight performance analysis for both propeller-driven and jet aircraft. The second edition features new content on vertical takeoff and landing, UAV launch, UAV recovery, use of rocket engine as the main engine, range for electric aircraft, electric engine, endurance for electric aircraft, gliding flight, pull-up, and climb-turn. In addition, this book includes end-of-chapter problems, MATLABĀ® code and examples, and case studies to enhance and reinforce student understanding.<br/><br/>This book is intended for senior undergraduate aerospace students taking courses in Aircraft Performance, Flight Dynamics, and Flight Mechanics.<br/><br/>Instructors will be able to utilize an updated Solutions Manual and Figure Slides for their course.
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Airplanes -- Performance
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Aerodynamics
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Home library Current library Date acquired Source of acquisition Cost, normal purchase price Full call number Accession Number Cost, replacement price Koha item type
        General Stacks PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 09/12/2024 2 10218.75 629.133 Sa15a2 A186599 13625.00 Books

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